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Study on Integrated Flight/Propulsion Control Method of Compound Adjustable Ducted Rocket

机译:化合物可调节管火箭综合飞行/推进方法研究

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For the integrated control of the missile and the compound adjustable ducted rocket, the Integrated Flight/Propulsion Control (1FPC) system was constructed by hierarchical dispersion method based on the mathematical model of the system and the coupling characteristics analysis between the subsystems. According to the work principle of the integrated system, the integration and the coordination of the subsystems were achieved by the motion control commands and the coordination control commands respectively. The IFPC method was validated by simulation based on typical mission. The results show that the IFPC system can control the motion of the missile and coordinate the operating status of the subsystems effectively.
机译:对于导弹的综合控制和化合物可调节的管道火箭,通过基于系统的数学模型和子系统之间的耦合特性分析,通过分层色散方法构建集成飞行/推进控制(1FPC)系统。根据集成系统的工作原理,分别通过运动控制命令和协调控制命令实现了子系统的集成和协调。基于典型任务的仿真验证了IFPC方法。结果表明,IFPC系统可以控制导弹的运动并有效地协调子系统的运行状态。

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